KR930023603A - Collector of compressor with irregular cross section - Google Patents

Collector of compressor with irregular cross section Download PDF

Info

Publication number
KR930023603A
KR930023603A KR1019930008558A KR930008558A KR930023603A KR 930023603 A KR930023603 A KR 930023603A KR 1019930008558 A KR1019930008558 A KR 1019930008558A KR 930008558 A KR930008558 A KR 930008558A KR 930023603 A KR930023603 A KR 930023603A
Authority
KR
South Korea
Prior art keywords
housing
collector
outlet
inlet
angular position
Prior art date
Application number
KR1019930008558A
Other languages
Korean (ko)
Inventor
레이몬드 와렌 매튜
Original Assignee
조운 이. 페더리시
프랙스에어 테크놀로지, 인코포레이티드
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 조운 이. 페더리시, 프랙스에어 테크놀로지, 인코포레이티드 filed Critical 조운 이. 페더리시
Publication of KR930023603A publication Critical patent/KR930023603A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/441Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • F04D29/444Bladed diffusers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/70Shape

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

본 발명은 원심펌프에 있어서, 날개가 있는 디퓨저에 대한 콜렉터에 관한것이며, 콜렉터 배출도관 입구에서 콜렉터 하우징의 방사상 단면적은 배출도관 입구면적의 40내지 80퍼센트이며, 배출도관 입구까지 유연하게 진행된다. 콜렉터 하우징에 있어서 단면적의 진행은 콜렉터 축방향 높이의 변화에 의해서 제공된다. 배출도관과 함께 이루는 교차점에서, 콜렉터는 축방향 높이로 단을 가지며, 이에 따라 유동이 콜렉터로 부터 배출도관 입구까지 적어도 부분적으로 원주방향을 향하게 된다.The present invention relates to a collector for a winged diffuser in a centrifugal pump, wherein the radial cross-sectional area of the collector housing at the collector outlet conduit inlet is 40 to 80 percent of the outlet conduit inlet area and proceeds flexibly to the outlet conduit inlet. Progression of the cross-sectional area in the collector housing is provided by a change in the collector axial height. At the intersection with the exhaust conduit, the collector has a stage at an axial height such that the flow is at least partially circumferentially from the collector to the outlet conduit inlet.

Description

비정형 단면을 갖는 압축기의 콜렉터Collector of compressor with irregular cross section

본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음Since this is an open matter, no full text was included.

제1도는 본 발명에 따른 원심 압축기의 축방향 단면도, 제2도는 제1도에 도시된 콜렉터 단면의 평면도, 제3도는 제2도에 표시된 대응하는 숫자의 화살표 방향을 따라 각각 도시한 단면도.1 is an axial sectional view of a centrifugal compressor according to the present invention, FIG. 2 is a plan view of the collector cross section shown in FIG. 1, and FIG. 3 is a cross sectional view along the direction of the arrow of the corresponding number shown in FIG.

Claims (10)

원심 압축기내의 날개가 있는 디퓨저에 사용되는 고효율의 콜렉터로서, a)원주상의 입구를 갖는 하우징으로서, 상기 원주상의 입구가 하우징의 내부 반경벽에 위치하고 상기 디퓨저의 출구를 감싸고 이 출구와 연결될수 있는 하우징과, 그리고 b) 상기 하우징으로 부터 나오는 배출도관으로서, 입구를 가지며, 이 입구에서 상기 하우징의 외부반경벽과 함께 예리한 교차점을 형성하는 배출도관을 포함하며, 상기 예리한 교차점과 방사상으로 정렬되는 제1각 위치에서, 상기 하우징이 상기 배출도관 입구면적의 40내지 80퍼센트의 방사상 단면적을 가지며, 이 방사상 단면적에서 상기 제1각 위치로 부터 상기 배출도관 입구로의 유연한 변이(transition)를 갖는 콜렉터.A high efficiency collector for a winged diffuser in a centrifugal compressor, comprising: a) a housing having a circumferential inlet, the circumferential inlet being located on an inner radial wall of the housing and surrounding the outlet of the diffuser and being connected to the outlet. B) an exhaust conduit exiting the housing, the exhaust conduit having an inlet, the exhaust conduit forming a sharp intersection with the outer radial wall of the housing, the radially aligned with the sharp intersection. In a first angular position, the housing has a radial cross-sectional area of 40 to 80 percent of the outlet conduit inlet area, the collector having a flexible transition from the first angular position to the outlet conduit inlet at this radial cross section; . 제1항에 있어서, 상기 하우징내의 의도된 원주상 유동방향에 따라 상기 예리한 교차점으로 부터 120°내지 320°의 참조각으로 측정된 제2각 위치에서, 상기 하우징이 상기 배출도관 입구 면적의 80 내지 100퍼센트와 동일한 단면적을 갖는 콜렉터.The housing of claim 1, wherein the housing is in the range of 80 to 80 of the exhaust conduit inlet area at a second angle position measured at a reference angle of 120 ° to 320 ° from the sharp intersection point along the intended circumferential flow direction within the housing. Collector with a cross section equal to 100 percent. 제1항에 있어서, 상기 하우징이 상기 제1각 위치로 부터 제2각 위치까지 일정한 방사상 폭과 증가되는 축방향 높이를 갖는 콜렉터.The collector of claim 1, wherein the housing has a constant radial width and an increased axial height from the first angular position to the second angular position. 제1항에 있어서, 상기 예리한 교차점과 방사상으로 정렬되는 상기 제1각 위치에서, 상기 하우징의 단면이 0.85 내지 1.25의 비율로 축방향 높이 및 방사상폭을 갖는 콜렉터.The collector of claim 1, wherein at the first angular position radially aligned with the sharp intersection, the cross section of the housing has an axial height and a radial width in a ratio of 0.85 to 1.25. 제1항에 있어서, 상기 하우징 단면의 중심의 방사상 위치가, 상기 제1각 위치에서 보다 20퍼센트를 넘지않게 증가하는 콜렉터.The collector of claim 1, wherein the radial position of the center of the housing cross-section increases by no more than 20 percent at the first angular position. 제1항에 있어서, 상기 하우징 단면의 중심이 상기 환형 하우징의 중심축으로 부터 일정한 방사상 거리에 위치하는 콜렉터.The collector of claim 1 wherein the center of the housing cross section is located at a constant radial distance from the central axis of the annular housing. 제1항에 있어서, 상기 하우징의 내부 반경벽이 상기 배출도관의 교차점에서 축방향 높이의 단을 가지며, 이것에 의하여 유동이 상기 하우징으로 부터 상기 배출도관내로 안내되고, 상기 하우징내에서의 유동의 재순환이 감소되는 콜렉터.2. The inner radial wall of claim 1 wherein the inner radial wall of the housing has an axial height end at the intersection of the discharge conduits, whereby flow is guided from the housing into the discharge conduit and flows within the housing. Collector with reduced recycling. 회전축, 이 회전축에 장착된 임펠러, 이 임펠러를 둘러싸는 익형의 디퓨저, 및 상기 임펠러를 둘러싸는 콜렉터를 포함하는 원심압축기로서, 상기 디퓨저가 상기 임펠러의 출구와 연결된 유입구, 및 배출구를 갖추고 잇으며, 상기 콜렉터가 a)원주상의 입구를 갖는 하우징으로서, 상기 원주상의 입구가 하우징의 내부반경벽에 위치하고 상기 날개가 있는 디퓨저의 출구를 감싸고 이출구와 연결될 수 있는 하우징과, 그리고 b) 상기 하우징으로 부터 나오는 배출도관으로서, 입구를 가지며, 이 입구에서 상기 하우징의 외부 반경벽과 함께 예리한 교차점을 형성하는 배출도관을 포함하며, 상기 예리한 교차점과 방사상으로 정렬되는 제1각 위치에서, 상기 하우징이 상기 배출도관 입구 면적의 40 내지 80퍼센트의 방사상 단면적을 가지며, 이 방사상 단면적에서 상기 제1원주상 위치로 부터 상기 배출도관 입구로의 유연한 변이를 갖는 압축기.A centrifugal compressor comprising a rotating shaft, an impeller mounted to the rotating shaft, an air diffuser surrounding the impeller, and a collector surrounding the impeller, the diffuser having an inlet connected to an outlet of the impeller, and an outlet, The collector is a) a housing having a circumferential inlet, the circumferential inlet being located on an inner radial wall of the housing and surrounding the outlet of the winged diffuser and connected to the outlet; and b) the housing An outlet conduit from the outlet, the outlet conduit having an inlet, the outlet conduit defining a sharp intersection with the outer radial wall of the housing, the first conduit radially aligned with the sharp intersection; Has a radial cross-sectional area of 40 to 80 percent of the outlet conduit inlet area, And a flexible transition from said first circumferential position to said outlet conduit inlet. 제8항에 있어서, 상기 콜렉터 하우징이 상기 제1각 위치로 부터 제2각 위치까지 일정한 방사상 폭 및 증가하는 축방향 높이를 갖는 압축기.9. The compressor of claim 8, wherein the collector housing has a constant radial width and increasing axial height from the first angular position to the second angular position. 제8항에 있어서, 상기 하우징 단면의 중심의 방사상 위치가 상기 제1각 위치에서 보다 20퍼센트를 넘지않게 증가하는 콜렉터.The collector of claim 8, wherein the radial position of the center of the housing cross-section increases no more than 20 percent than at the first angular position. ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.※ Note: The disclosure is based on the initial application.
KR1019930008558A 1992-05-20 1993-05-19 Collector of compressor with irregular cross section KR930023603A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/885,860 US5266003A (en) 1992-05-20 1992-05-20 Compressor collector with nonuniform cross section
US7/885,860 1992-05-20

Publications (1)

Publication Number Publication Date
KR930023603A true KR930023603A (en) 1993-12-21

Family

ID=25387849

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019930008558A KR930023603A (en) 1992-05-20 1993-05-19 Collector of compressor with irregular cross section

Country Status (8)

Country Link
US (1) US5266003A (en)
EP (1) EP0570955A1 (en)
JP (1) JPH0633898A (en)
KR (1) KR930023603A (en)
CN (1) CN1080032A (en)
BR (1) BR9301942A (en)
CA (1) CA2096555A1 (en)
MX (1) MX9302934A (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4892832A (en) * 1986-12-05 1990-01-09 Toppan Printing Co., Ltd. Filter bag for microbiological examination
US5669756A (en) * 1996-06-07 1997-09-23 Carrier Corporation Recirculating diffuser
US5971023A (en) * 1997-02-12 1999-10-26 Medtronic, Inc. Junction for shear sensitive biological fluid paths
US7014422B2 (en) * 2003-06-13 2006-03-21 American Standard International Inc. Rounded blower housing with increased airflow
US7448852B2 (en) * 2005-08-09 2008-11-11 Praxair Technology, Inc. Leaned centrifugal compressor airfoil diffuser
WO2007033199A2 (en) * 2005-09-13 2007-03-22 Ingersoll-Rand Company Volute for a centrifugal compressor
EP2068002A1 (en) * 2007-12-07 2009-06-10 ABB Turbo Systems AG Compressor casing
JP5720267B2 (en) * 2011-01-21 2015-05-20 株式会社Ihi Centrifugal compressor
US9200639B2 (en) * 2012-08-19 2015-12-01 Honeywell International Inc. Compressor housing assembly
JP6379568B2 (en) * 2014-03-26 2018-08-29 株式会社Ihi Scroll and turbo compressor
DE102016102924A1 (en) * 2016-02-19 2017-08-24 Abb Turbo Systems Ag Diffuser of a centrifugal compressor
JP6876146B2 (en) * 2017-11-20 2021-05-26 三菱重工エンジン&ターボチャージャ株式会社 Centrifugal compressor and turbocharger equipped with this centrifugal compressor

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1670065A (en) * 1926-05-08 1928-05-15 Gen Electric Centrifugal pump and compressor
US2373713A (en) * 1942-05-20 1945-04-17 Gen Electric Centrifugal compressor
US2361521A (en) * 1943-11-01 1944-10-31 W S Darley & Company Centrifugal pump
CH310602A (en) * 1948-09-25 1955-10-31 Buechi Alfred Method and device for flushing and charging internal combustion engines.
US2864552A (en) * 1954-08-18 1958-12-16 Sir George Godfrey & Partners Shaft or like bearings
FR1122467A (en) * 1955-03-02 1956-09-07 Anciens Ets Brissonneau & Lotz Method and machine for gas compression
US2999628A (en) * 1957-08-26 1961-09-12 Joseph S Crombie Low pressure compressor
US2897917A (en) * 1957-11-15 1959-08-04 Fairchild Engine & Airplane Apparatus for separating moisture and condensable vapors from a gas
US3301472A (en) * 1965-01-14 1967-01-31 American Radiator & Standard Blower
US3635579A (en) * 1970-02-26 1972-01-18 Westinghouse Electric Corp Discharge nozzle arrangement for centrifugal gas compressor
GB1430308A (en) * 1973-04-06 1976-03-31 Woollenweber W E Rotatable assembly
JPS5045307A (en) * 1973-08-18 1975-04-23
US3922108A (en) * 1974-03-18 1975-11-25 Wallace Murray Corp Pre-whirl turbo charger apparatus
US4181466A (en) * 1977-03-17 1980-01-01 Wallace Murray Corp. Centrifugal compressor and cover
JPS5421608A (en) * 1977-07-18 1979-02-19 Sanyo Electric Co Ltd Centrifugal fan
US4213742A (en) * 1977-10-17 1980-07-22 Union Pump Company Modified volute pump casing
IN152940B (en) * 1978-10-20 1984-05-05 Cummins Engine Co Inc
US4240678A (en) * 1979-02-22 1980-12-23 Wallace Murray Corporation Non-rotating fluid damped combination thrust and journal bearing
US4396348A (en) * 1979-03-27 1983-08-02 Aeplc Viscosity pump
DE3001868C2 (en) * 1980-01-19 1984-01-19 Klein, Schanzlin & Becker Ag, 6710 Frankenthal Centrifugal pump with double volute casing
DE3325756C1 (en) * 1983-07-16 1984-09-13 Aktiengesellschaft Kühnle, Kopp & Kausch, 6710 Frankenthal Adjustable nozzle
NZ211792A (en) * 1984-04-18 1986-09-10 Warman Int Ltd Centrifugal pump casing
EP0305879B1 (en) * 1987-09-01 1993-07-21 Hitachi, Ltd. Diffuser for centrifugal compressor
US4859145A (en) * 1987-10-19 1989-08-22 Sundstrand Corporation Compressor with supercritical diffuser
ATE96207T1 (en) * 1989-01-19 1993-11-15 Ebara Corp PUMP HOUSING.
WO1990009524A1 (en) * 1989-02-14 1990-08-23 Airflow Research & Manufacturing Corporation Centrifugal fan and diffuser with accumulating volute
US4900225A (en) * 1989-03-08 1990-02-13 Union Carbide Corporation Centrifugal compressor having hybrid diffuser and excess area diffusing volute
US4938664A (en) * 1989-11-13 1990-07-03 Carrier Corporation Oil reclaim system

Also Published As

Publication number Publication date
CA2096555A1 (en) 1993-11-21
JPH0633898A (en) 1994-02-08
CN1080032A (en) 1993-12-29
MX9302934A (en) 1994-07-29
US5266003A (en) 1993-11-30
EP0570955A1 (en) 1993-11-24
BR9301942A (en) 1993-11-30

Similar Documents

Publication Publication Date Title
US3333762A (en) Diffuser for centrifugal compressor
US7628583B2 (en) Discrete passage diffuser
US3420435A (en) Diffuser construction
US4781530A (en) Compressor range improvement means
US6279322B1 (en) Deswirler system for centrifugal compressor
US3243102A (en) Centrifugal fluid pump
US5257906A (en) Exhaust system for a turbomachine
SU1486067A3 (en) Axial-flow air-blower
US3719430A (en) Diffuser
US6695579B2 (en) Diffuser having a variable blade height
US4100732A (en) Centrifugal compressor advanced dump diffuser
RU95112478A (en) SPIRAL HOUSING FOR TURBO MACHINES
KR930004642A (en) Centrifugal compressor with high efficiency and wide operating
US2991927A (en) Apparatus for moving fluids
US3986791A (en) Hydrodynamic multi-stage pump
KR930023603A (en) Collector of compressor with irregular cross section
EP0267725A2 (en) Axial flow fan
EP0602007B1 (en) Vacuum cleaner having an impeller and diffuser
US3905721A (en) Centrifugal compressor diffuser
US3307776A (en) Fluid-working machines
US3059833A (en) Fans
US3743436A (en) Diffuser for centrifugal compressor
US4913621A (en) Centrifugal fan
US4564334A (en) Guide wheel for multistage centrifugal pumps
US4382747A (en) Compressor of a turbocharger

Legal Events

Date Code Title Description
A201 Request for examination
E902 Notification of reason for refusal
E601 Decision to refuse application